EP4621235A1 - Thrust support mechanism - Google Patents
Thrust support mechanismInfo
- Publication number
- EP4621235A1 EP4621235A1 EP23891509.4A EP23891509A EP4621235A1 EP 4621235 A1 EP4621235 A1 EP 4621235A1 EP 23891509 A EP23891509 A EP 23891509A EP 4621235 A1 EP4621235 A1 EP 4621235A1
- Authority
- EP
- European Patent Office
- Prior art keywords
- pressure chamber
- receiving mechanism
- fluid
- low
- scroll
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Withdrawn
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04C—ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
- F04C18/00—Rotary-piston pumps specially adapted for elastic fluids
- F04C18/02—Rotary-piston pumps specially adapted for elastic fluids of arcuate-engagement type, i.e. with circular translatory movement of co-operating members, each member having the same number of teeth or tooth-equivalents
- F04C18/0207—Rotary-piston pumps specially adapted for elastic fluids of arcuate-engagement type, i.e. with circular translatory movement of co-operating members, each member having the same number of teeth or tooth-equivalents both members having co-operating elements in spiral form
- F04C18/0215—Rotary-piston pumps specially adapted for elastic fluids of arcuate-engagement type, i.e. with circular translatory movement of co-operating members, each member having the same number of teeth or tooth-equivalents both members having co-operating elements in spiral form where only one member is moving
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04C—ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
- F04C29/00—Component parts, details or accessories of pumps or pumping installations, not provided for in groups F04C18/00 - F04C28/00
- F04C29/0021—Systems for the equilibration of forces acting on the pump
- F04C29/0028—Internal leakage control
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04C—ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
- F04C29/00—Component parts, details or accessories of pumps or pumping installations, not provided for in groups F04C18/00 - F04C28/00
- F04C29/0042—Driving elements, brakes, couplings, transmissions specially adapted for pumps
- F04C29/005—Means for transmitting movement from the prime mover to driven parts of the pump, e.g. clutches, couplings, transmissions
- F04C29/0057—Means for transmitting movement from the prime mover to driven parts of the pump, e.g. clutches, couplings, transmissions for eccentric movement
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04C—ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
- F04C2240/00—Components
- F04C2240/40—Electric motor
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04C—ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
- F04C2240/00—Components
- F04C2240/50—Bearings
Definitions
- the present invention relates to a thrust receiving mechanism, for example, a thrust receiving mechanism used in a rotating machine including an eccentric mechanism.
- Machines that are rotationally driven and that are used in various industrial fields include not only a rotating machine in which a central shaft rotates while being held at a fixed position, but also a rotating machine that a central shaft rotates eccentrically.
- a rotating machine that rotates eccentrically is a scroll compressor or the like, and this type of compressor includes a scroll compression mechanism composed of a fixed scroll including a scroll wrap on a surface of an end plate and a movable scroll including a scroll wrap on a surface of an end plate, an eccentric mechanism for eccentrically rotating a rotating shaft, and the like, and has a mechanism for pressurizing a fluid supplied from a low-pressure chamber on a radial outer side of both the scrolls and discharging high-pressure fluid from a discharge hole, which is formed at the center of the fixed scroll, by sliding the movable scroll relative to the fixed scroll while eccentrically rotating the movable scroll due to the rotation of the rotating shaft.
- the scroll compressor using the mechanism for sliding the movable scroll relative to the fixed scroll while eccentrically rotating the movable scroll not only has high compression efficiency, but also is low noise, the scroll compressor is widely used in, for example, a refrigeration cycle and the like; however, leakage of a refrigerant from an axial gap between both scrolls increases, which is a problem.
- a thrust bearing is disposed on a back surface side of a movable scroll, and a ring-shaped plate is disposed in the thrust bearing.
- a plurality of spiral groove mechanisms are formed independently in a circumferential direction on a surface on a movable scroll side of the ring-shaped plate.
- a plurality of grooves are provided in a substantially radial shape toward a land at the center of each spiral groove mechanism is provided in the spiral groove mechanism.
- each groove extends in a radial direction from the land at the center while inclining in a counterclockwise direction, one end on a land side of the groove is tapered, and the other end on the side opposite to the land is wider than the one end.
- the movable scroll moves from the other end of the groove toward the one end during eccentric rotation. Accordingly, a fluid on a radial outer side or a radial inner side of the ring-shaped plate is taken into the groove, and dynamic pressure is generated in the vicinity of the one end of the groove. Accordingly, slidability can be increased by forming a fluid film between sliding surfaces of the movable scroll and the ring-shaped plate while keeping the sliding surfaces apart from each other, and leakage of the refrigerant from an axial gap between both the scrolls can be reduced by pressing the movable scroll against the fixed scroll.
- a fluid on the low-pressure side is directed toward the high-pressure side by each groove, and a fluid on the high-pressure side outside the sliding surfaces is less likely to enter a gap between the sliding surfaces. For that reason, leakage of the fluid on the high-pressure side to the low-pressure side can be suppressed.
- the fluid that has flowed out from the first groove into the gap between the sliding surfaces can be stored in the buffer space, and the fluid can be supplied from the buffer space to the second groove.
- the buffer space is a depression. According to this preferable configuration, the fluid in the buffer space can more reliably generate dynamic pressure in the second groove without being affected by the axial positions of the thrust receiving mechanism and the movable scroll.
- the depression communicatees with the low-pressure side. According to this preferable configuration, the fluid in the depression does not run out, and stable slidability can be achieved.
- each of the dynamic pressure generation portions has a diameter smaller than a diameter of the thrust receiving mechanism, and the dynamic pressure generation portions are disposed at equal spacings in a circumferential direction of the thrust receiving mechanism. According to this preferable configuration, leakage of the fluid on the high-pressure side to the low-pressure side in the circumferential direction can be suppressed.
- a thrust receiving mechanism according to a first embodiment of the present invention will be described with reference to FIGS. 1 to 5 .
- the thrust receiving mechanism according to the first embodiment of the present invention is applied to a rotating machine including an eccentric mechanism, for example, a scroll compressor C that suctions, compresses, and discharges a refrigerant serving as a fluid used in an air conditioning system of an automobile or the like.
- the refrigerant is a gas, and is mixed with lubricating oil in the form of mist.
- the scroll compressor C is mainly composed of a housing 1; a rotating shaft 2; an inner casing 3; a scroll compression mechanism 4; a side seal 7; a thrust plate 8 serving as the thrust receiving mechanism; and a drive motor M.
- the housing 1 is composed of a casing 11 having a cylindrical shape, and a cover 12 that closes an opening of the casing 11. An opening of the casing 11 on the side axially opposite to the opening closed by the cover 12 is closed by the drive motor M.
- a low-pressure chamber 20 serving as an external space on a low-pressure side to which low-pressure refrigerant is supplied from a refrigerant circuit (not illustrated) through a suction port 10
- a high-pressure chamber 30 from which high-pressure refrigerant compressed by the scroll compression mechanism 4 is discharged
- a back pressure chamber 50 serving as an external space on a high-pressure side to which some of the refrigerant compressed by the scroll compression mechanism 4 is supplied together with the lubricating oil are formed.
- the back pressure chamber 50 is formed inside the inner casing 3 having a cylindrical shape that is accommodated inside the casing 11.
- a discharge communication passage 13 communicating between the refrigerant circuit (not illustrated) and the high-pressure chamber 30 is formed in the cover 12.
- a part of a back pressure communication passage 14 communicating between the high-pressure chamber 30 and the back pressure chamber 50 is formed in the cover 12 by branching off from the discharge communication passage 13.
- an oil separator 6 that separates the lubricating oil from the refrigerant is provided in the discharge communication passage 13.
- the inner casing 3 is fixed in a state where an axial end portion of the inner casing 3 abuts against an end plate 41a of a fixed scroll 41 constituting the scroll compression mechanism 4.
- a suction communication passage 15 is formed in a side wall of the inner casing 3 so as to penetrate therethrough in a radial direction.
- the low-pressure chamber 20 is formed from the outside of the inner casing 3 to the inside of the inner casing 3 via the suction communication passage 15.
- the refrigerant supplied to the inside of the inner casing 3 through the suction communication passage 15 is suctioned into the scroll compression mechanism 4.
- the scroll compression mechanism 4 is mainly composed of the fixed scroll 41 fixed to the cover 12 in a sealed manner, and the movable scroll 42 accommodated inside the inner casing 3.
- the fixed scroll 41 is made of metal, and includes a scroll wrap 41b protruding from a surface of the end plate 41a having a disk shape, namely, from the end plate 41a toward the movable scroll 42.
- a recess 41c formed by recessing a radial inner side of a back surface of the end plate 41a, namely, an end surface of the end plate 41a in a direction opposite to the cover 12, the end surface abutting against the cover 12, is formed in the fixed scroll 41, and the high-pressure chamber 30 is defined by the recess 41c and the cover 12.
- the movable scroll 42 is made of metal, and includes a scroll wrap 42b protruding from a surface of an end plate 42a having a disk shape, namely, from the end plate 42a toward the fixed scroll 41.
- a boss 42c protruding from the center of a back surface of the end plate 42a is formed on the movable scroll 42.
- An eccentric portion 2a formed on the rotating shaft 2 is inserted into the boss 42c so as to be capable of relative rotation.
- the eccentric portion 2a of the rotating shaft 2 and a counterweight portion 2b protruding from the rotating shaft 2 in a radially outward direction constitute an eccentric mechanism that eccentrically rotates the rotating shaft 2.
- the eccentric portion 2a rotates eccentrically, and the movable scroll 42 slides relative to the fixed scroll 41 in a state where the movable scroll 42 maintains the posture with respect to the fixed scroll 41 while rotating eccentrically.
- the movable scroll 42 rotates eccentrically with respect to the fixed scroll 41, and the contact position between the wraps 41b and 42b moves sequentially in a rotation direction along with this rotation, and a compression chamber 40 formed between the wraps 41b and 42b is gradually reduced while moving toward the center.
- the refrigerant suctioned into the compression chamber 40 from the low-pressure chamber 20 formed on the radial outer side of the scroll compression mechanism 4 is compressed, and finally, the high-pressure refrigerant is discharged into the high-pressure chamber 30 through a discharge hole 41d provided at the center of the fixed scroll 41.
- the side seal 7 is made of resin, has a rectangular cross section and an annular shape when viewed in an axial direction, and is fixed to the back surface of the end plate 42a of the movable scroll 42.
- a sliding surface 7a that abuts against a sliding surface 8a (refer to FIG. 1 ) formed on the thrust plate 8 is formed on the side seal 7.
- the sliding surface 7a is a flat surface, and constitutes a back surface-side sliding surface of the movable scroll 42.
- the thrust plate 8 As illustrated in FIGS. 1 and 2 , the thrust plate 8 is made of metal, and has an annular shape.
- the thrust plate 8 is composed of a plurality of dynamic pressure generation portions 81 (16 pieces in the present embodiment) and a plurality of connecting portions 82 (16 pieces in the present embodiment).
- the dynamic pressure generation portions 81 adjacent to each other in a circumferential direction are connected by the connecting portions 82.
- Each connecting portion 82 has the same thickness as a base portion 83 of each dynamic pressure generation portion 81, and has a smaller radial width than the base portion 83. Namely, the dynamic pressure generation portion 81 bulges further toward the radial inner side and the radial outer side of the thrust plate 8 than the connecting portion 82.
- the dynamic pressure generation portion 81 and the connecting portion 82 form a step portion on each of the radial inner side and the radial outer side.
- these step portions will be simply referred to as "step portions between the dynamic pressure generation portion 81 and the connecting portion 82".
- the dynamic pressure generation portion 81 includes the base portion 83; a depression 84 serving as a buffer space; a first inclined groove group 85 serving as first grooves; and a second inclined groove group 86 severing as second grooves.
- a depression 84 serving as a buffer space
- a first inclined groove group 85 serving as first grooves
- a second inclined groove group 86 severing as second grooves.
- the base portion 83 has a circular shape when viewed in the axial direction.
- the depression 84 is formed at a central portion of the base portion 83, namely, between a radial inner end and a radial outer end of the thrust plate 8 to be open toward a sliding surface 8a side.
- the depression 84 is a bottomed recess having a circular shape when viewed in the axial direction.
- the first inclined groove group 85 is provided on the sliding surface 8a side of the base portion 83 to be closer to a low-pressure chamber 20 side than the depression 84.
- the first inclined groove group 85 is composed of a plurality of first inclined grooves 851 (eight pieces in the present embodiment).
- Each first inclined groove 851 extends from one end 851a on the low-pressure chamber 20 side toward the other end 851b on a back pressure chamber 50 side while inclining toward one side in the circumferential direction (in the present embodiment, a counterclockwise direction in FIG. 2 ).
- the one end 851a communicates with the low-pressure chamber 20, and the other end 851b is a closed end portion.
- the other end 851b of the first inclined groove 851 and the depression 84 are partitioned off from each other by a land.
- the second inclined groove group 86 is provided on the sliding surface 8a side of the base portion 83 to be closer to the back pressure chamber 50 side than the depression 84.
- the second inclined groove group 86 is composed of a plurality of second inclined grooves 861 (eight pieces in the present embodiment).
- Each second inclined groove 861 extends from one end 861a on the low-pressure chamber 20 side toward the other end 861b on the back pressure chamber 50 side while inclining toward the one side in the circumferential direction (in the present embodiment, the counterclockwise direction in FIG. 2 ).
- the one end 861a communicates with the depression 84, and the other end 861b is a closed end portion.
- the other end 861b of the second inclined groove 861 is partitioned off from the back pressure chamber 50 or the second inclined grooves 861 by the land. Namely, each second inclined groove 861 does not communicate with the back pressure chamber 50.
- the thrust plate 8 is fitted into an installation groove 3b provided in the inner casing 3.
- An inner wall constituting the installation groove 3b has a shape that is substantially similar to and slightly larger than the outer shape of the thrust plate 8, and by engaging the step portions between the dynamic pressure generation portions 81 and the connecting portions 82 with the inner wall, the rotation of the thrust plate 8 in the circumferential direction is restricted.
- a seal ring 43 (refer to FIG. 1 ) is fixed to a back surface of the thrust plate 8.
- the seal ring 43 abuts against a bottom surface of the installation groove 3b of the inner casing 3. Accordingly, the thrust plate 8 functions as a thrust receiving mechanism that receives an axial load of the movable scroll 42 via the side seal 7.
- the side seal 7 and the seal ring 43 partition the low-pressure chamber 20 formed on the radial outer side of the movable scroll 42 and the back pressure chamber 50 formed on a back surface side of the movable scroll 42 off from each other inside the inner casing 3.
- the back pressure chamber 50 is formed as a sealed space by sealing a gap between a through-hole 3a and the rotating shaft 2 inserted into the through-hole 3a with a seal ring 44 fixed to an inner periphery of the through-hole 3a provided at the center of the inner casing 3.
- an orifice (not illustrated) is provided in the back pressure communication passage 14 that is formed through the cover 12, the fixed scroll 41, and the inner casing 3, and that communicates between the high-pressure chamber 30 and the back pressure chamber 50, and the refrigerant in the high-pressure chamber 30, of which the pressure is adjusted to be reduced by the orifice, is supplied to the back pressure chamber 50, together with the lubricating oil separated by the oil separator 6. At this time, the pressure in the back pressure chamber 50 is adjusted to be higher than the pressure in the low-pressure chamber 20.
- a pressure relief hole 16 penetrating through the inner casing 3 in the radial direction and communicating between the low-pressure chamber 20 and the back pressure chamber 50 is formed in the inner casing 3, and a pressure adjustment valve 45 is provided in the pressure relief hole 16.
- the pressure adjustment valve 45 opens when the pressure in the back pressure chamber 50 becomes higher than a set value.
- the boss 42c of the movable scroll 42 is inserted into a through-hole 8b at the center of the thrust plate 8.
- the through-hole 8b is formed with a diameter large enough to allow eccentric rotation of the eccentric portion 2a of the rotating shaft 2 that is inserted into the boss 42c.
- the sliding surface 7a of the side seal 7 is slidable relative to the sliding surface 8a of the thrust plate 8 while rotating eccentrically due to the eccentric rotation of the rotating shaft 2 (refer to FIG. 3 ).
- FIGS. 3B to 3D illustrate states where the boss 42c has rotated by 90 degrees, 180 degrees, and 270 degrees, respectively, with FIG. 3A as a reference for the counterclockwise direction, along a rotation trajectory of the boss 42c indicated by a black arrow when viewed from a fixed scroll 41 side.
- a sliding region between the sliding surface 7a of the side seal 7 and the sliding surface 8a of the thrust plate 8 is schematically illustrated by dots.
- the rotating shaft 2 only the eccentric portion 2a inserted into the boss 42c is illustrated, and the illustration of the counterweight portion 2b and the like constituting the eccentric mechanism is omitted.
- the thrust plate 8 has the sliding surface 8a that slides relative to the sliding surface 7a of the side seal 7 that rotates eccentrically.
- an elastic member 9 (refer to FIG. 1 ) is inserted between the side seal 7 and the scroll compression mechanism 4, in detail, between the side seal 7 and the movable scroll 42, and dynamic pressure generated between the side seal 7 and the thrust plate 8 absorbs a difference in axial position in the circumferential phase, namely, prevents the movable scroll 42 from tilting.
- the elastic member 9 may be made of a deformable material, such as an O-ring, or may be deformable in shape, such as a spring.
- FIGS. 4 and 5 a sliding state between one dynamic pressure generation portion 81A of the thrust plate 8 located at 12 o'clock in FIG. 3 and the side seal 7 will be described as an example.
- FIG. 4 illustrates a mode when the side seal 7 moves with respect to the one dynamic pressure generation portion 81A from the state illustrated in FIG. 3A toward the state illustrated in FIG. 3B .
- FIG. 5 illustrates a mode when the side seal 7 moves with respect to the one dynamic pressure generation portion 81A from the state illustrated in FIG. 3C toward the state illustrated in FIG. 3D .
- the side seal 7 overlaps the first inclined groove group 85 of the one dynamic pressure generation portion 81A in the axial direction. At this time, the side seal 7 slides counterclockwise relative to the dynamic pressure generation portion 81A.
- a fluid F1 in the low-pressure chamber 20 that is present in each first inclined groove 851 of the first inclined groove group 85 moves from the one end 851a toward the other end 851b (refer to black arrows in FIG. 4 ).
- the fluid F1 that has flowed out from the other end 851b into a gap between the sliding surfaces 7a and 8a moves toward the back pressure chamber 50 side. Accordingly, a fluid F2 in the back pressure chamber 50 is pushed back toward the back pressure chamber 50 side, and is less likely to flow into the gap between the sliding surfaces 7a and 8a (refer to white arrows in FIG. 4 ). In addition, some of the fluid F1 and some of the fluid F2 are stored in the depression 84.
- the side seal 7 overlaps the second inclined groove group 86 of the one dynamic pressure generation portion 81A in the axial direction. At this time, the side seal 7 slides counterclockwise relative to the dynamic pressure generation portion 81A.
- each second inclined groove 861 of the second inclined groove group 86 moves from the one end 861a toward the other end 861b (refer to black arrows in FIG. 5 ).
- the depression 84 gradually ceases to communicate with the back pressure chamber 50 side, and begins to communicate with the low-pressure chamber 20 side, so that the amount of the fluid F1 in the low-pressure chamber 20 in the fluid supplied from the depression 84 to the second inclined grooves 861 gradually increases, and in the state illustrated in FIG. 5 , almost all of the supplied fluid is the fluid F1.
- the fluid F1 that has flowed out from the other end 861b into the gap between the sliding surfaces 7a and 8a moves toward the back pressure chamber 50 side. Accordingly, the fluid F2 in the back pressure chamber 50 is pushed back toward the back pressure chamber 50 side, and is less likely to flow into the gap between the sliding surfaces 7a and 8a (refer to white arrows in FIG. 5 ).
- the thrust plate 8 includes the dynamic pressure generation portions 81, each including the first inclined groove group 85 located on the low-pressure chamber 20 side and the second inclined groove group 86 located on the back pressure chamber 50 side, and the second inclined grooves 861 of the second inclined groove group 86 do not communicate with the back pressure chamber 50 side. According to this configuration, since the fluid F2 in the back pressure chamber 50 that has higher pressure than the fluid F1 in the low-pressure chamber 20 is restricted from entering the gap between the sliding surfaces 7a and 8a, leakage of the fluid F2 into the low-pressure chamber 20 can be suppressed.
- the depression 84 serving as a buffer space is formed between the first inclined groove group 85 and the second inclined groove group 86, the fluid F1 that has flowed out from the first inclined groove group 85 into the gap between the sliding surfaces 7a and 8a can be stored in the depression 84, and the fluid F1 can be supplied from the depression 84 to the second inclined groove group 86.
- the fluid F1 can be smoothly supplied from the low-pressure chamber 20 to the first inclined grooves 851.
- the thrust plate 8 is configured such that the plurality of dynamic pressure generation portions 81 are connected in an annular shape such that each second inclined groove group 86 is located on the back pressure chamber 50 side. According to this configuration, leakage of the fluid F2 in the back pressure chamber 50 to the low-pressure chamber 20 side in the circumferential direction can be suppressed.
- the mode in which the communication groove 287 is a recessed groove that is open to the sliding surface 28a side has been provided as an example; however, the present invention is not limited to this mode, and a hole that communicates between a side surface on the low-pressure chamber 20 side of the depression 284 and a side surface on the low-pressure chamber 20 side of the thrust plate 28 may be provided.
- the mode in which all the second inclined grooves 861 of the second inclined groove group 86 do not communicate with the back pressure chamber 50 side has been provided as an example; however, some of the second inclined grooves 861 may communicate with the back pressure chamber.
- the number of the inclined grooves not communicating with the back pressure chamber is larger than the number of the inclined grooves communicating with the back pressure chamber.
- the mode in which the first grooves and the second grooves are inclined grooves has been provided as an example; however, the first grooves and the second grooves may not be inclined grooves. Namely, any groove may be implemented as long as the groove can generate dynamic pressure, and a known structure capable of generating dynamic pressure, such as a groove extending parallel to the circumferential direction or a groove of which the bottom surface is inclined, may be used.
- the mode in which the thrust plate of the first and second embodiments is configured such that the plurality of dynamic pressure generation portions are connected in the circumferential direction to form an annular shape has been provided as an example; however, at least one dynamic pressure generation portion may be provided.
- the thrust plate is not limited to having an annular shape.
- the mode in which the depression serving as a buffer space is formed in the thrust plate has been provided as an example; however, a buffer space such as a depression may be formed on a side seal side. Incidentally, the buffer space may not be provided between the first inclined groove group and the second inclined groove group.
- the mode in which the inclined grooves of the second inclined groove group communicate with the depression has been provided as an example; however, dimples or the like not communicating with the depression may be implemented.
- the mode in which the inclined grooves of the first inclined groove group communicate with the low-pressure chamber has been provided as an example; however, dimples or the like not communicating with the low-pressure chamber may be implemented.
- the mode in which the thrust plate serving as a thrust receiving mechanism is applied to the scroll compressor C used in an air conditioning system of an automobile or the like has been described; however, the present invention is not limited to this mode, and may be applied to, for example, a scroll expander-compressor or the like in which an expander and a compressor are integrally provided as long as the scroll expander-compressor is a rotating machine including an eccentric mechanism.
- the radial outer side and the radial inner side of the thrust plate have been described as the low-pressure side and the high-pressure side, respectively; however, the radial outer side and the radial inner side of the thrust plate may be the high-pressure side and the low-pressure side, respectively.
- the fluid present in the spaces inside and outside the sliding surface of the thrust receiving mechanism may be any of gas, liquid, and a mixture of gas and liquid.
- the side seal and the thrust plate having the sliding surfaces that slide relative to each other have been described as being made of resin and metal, respectively; however, the material of the thrust receiving mechanism may be freely selected depending on the usage environment or the like.
- the mode in which the side seal slides relative to the thrust plate has been provided as an example; however, the back surface of the movable scroll may directly slide relative to the thrust plate.
- the mode in which the thrust plate is disposed in a state where the thrust plate is restricted from rotating by being fitted to the installation groove provided in the inner casing has been provided as an example; however, the present invention is not limited to this mode, and for example, the thrust plate may be non-rotatably fixed to the inner casing by bolts or the like.
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Rotary Pumps (AREA)
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP2022184400 | 2022-11-17 | ||
| PCT/JP2023/040690 WO2024106362A1 (ja) | 2022-11-17 | 2023-11-13 | スラスト受機構 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| EP4621235A1 true EP4621235A1 (en) | 2025-09-24 |
Family
ID=91084704
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| EP23891509.4A Withdrawn EP4621235A1 (en) | 2022-11-17 | 2023-11-13 | Thrust support mechanism |
Country Status (6)
| Country | Link |
|---|---|
| US (1) | US20260022700A1 (https=) |
| EP (1) | EP4621235A1 (https=) |
| JP (1) | JPWO2024106362A1 (https=) |
| KR (1) | KR20250041053A (https=) |
| CN (1) | CN119790228A (https=) |
| WO (1) | WO2024106362A1 (https=) |
Citations (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH09317666A (ja) | 1996-05-31 | 1997-12-09 | Matsushita Electric Ind Co Ltd | スクロール圧縮機 |
Family Cites Families (23)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS6093192A (ja) * | 1983-10-27 | 1985-05-24 | Matsushita Electric Ind Co Ltd | スクロ−ル圧縮機 |
| JPH0647991B2 (ja) * | 1986-05-15 | 1994-06-22 | 三菱電機株式会社 | スクロ−ル圧縮機 |
| JPH01300080A (ja) * | 1988-05-30 | 1989-12-04 | Matsushita Refrig Co Ltd | スクロールコンプレッサ |
| JPH0486301A (ja) * | 1990-07-30 | 1992-03-18 | Mitsubishi Heavy Ind Ltd | スクロール型流体機械 |
| CA2170746C (en) * | 1993-09-01 | 2005-01-25 | Josef Sedy | Face seal with angled and annular grooves |
| JPH07208356A (ja) * | 1994-01-04 | 1995-08-08 | Hitachi Ltd | スクロール圧縮機 |
| US6146119A (en) * | 1997-11-18 | 2000-11-14 | Carrier Corporation | Pressure actuated seal |
| JP3965982B2 (ja) * | 2001-11-29 | 2007-08-29 | 松下電工株式会社 | スクロール型ポンプ |
| JP2004028017A (ja) * | 2002-06-27 | 2004-01-29 | Denso Corp | スクロール型圧縮機 |
| KR100547331B1 (ko) * | 2004-01-09 | 2006-01-26 | 엘지전자 주식회사 | 스크롤 압축기 |
| JP2006138243A (ja) * | 2004-11-11 | 2006-06-01 | Sanden Corp | スクロール型圧縮機 |
| US20070092390A1 (en) * | 2005-10-26 | 2007-04-26 | Copeland Corporation | Scroll compressor |
| JP5181534B2 (ja) * | 2007-05-22 | 2013-04-10 | パナソニック株式会社 | スクロール圧縮機 |
| JP2009047040A (ja) * | 2007-08-17 | 2009-03-05 | Mitsubishi Heavy Ind Ltd | スクロール型流体機械 |
| JP4951586B2 (ja) * | 2008-05-30 | 2012-06-13 | 日立アプライアンス株式会社 | スクロール流体機械 |
| JP5310251B2 (ja) * | 2009-05-18 | 2013-10-09 | 信越化学工業株式会社 | 非水電解質二次電池用負極材の製造方法 |
| JP6488893B2 (ja) * | 2015-06-05 | 2019-03-27 | 富士電機株式会社 | スクロール圧縮機 |
| KR102203051B1 (ko) * | 2016-08-02 | 2021-01-14 | 이구루코교 가부시기가이샤 | 밀봉 장치 |
| US10718333B2 (en) * | 2017-06-16 | 2020-07-21 | Trane International Inc. | Aerostatic thrust bearing method and method of aerostatically supporting a thrust load in a scroll compressor |
| CN115917192A (zh) * | 2020-07-06 | 2023-04-04 | 伊格尔工业股份有限公司 | 滑动部件 |
| JP7497132B2 (ja) * | 2020-07-06 | 2024-06-10 | イーグル工業株式会社 | 摺動部品 |
| KR102841101B1 (ko) * | 2020-07-06 | 2025-07-31 | 이구루코교 가부시기가이샤 | 슬라이딩 부품 |
| WO2022009768A1 (ja) * | 2020-07-06 | 2022-01-13 | イーグル工業株式会社 | 摺動部品 |
-
2023
- 2023-11-13 EP EP23891509.4A patent/EP4621235A1/en not_active Withdrawn
- 2023-11-13 WO PCT/JP2023/040690 patent/WO2024106362A1/ja not_active Ceased
- 2023-11-13 US US19/106,562 patent/US20260022700A1/en active Pending
- 2023-11-13 KR KR1020257006467A patent/KR20250041053A/ko active Pending
- 2023-11-13 CN CN202380062022.8A patent/CN119790228A/zh active Pending
- 2023-11-13 JP JP2024558843A patent/JPWO2024106362A1/ja active Pending
Patent Citations (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH09317666A (ja) | 1996-05-31 | 1997-12-09 | Matsushita Electric Ind Co Ltd | スクロール圧縮機 |
Also Published As
| Publication number | Publication date |
|---|---|
| US20260022700A1 (en) | 2026-01-22 |
| JPWO2024106362A1 (https=) | 2024-05-23 |
| KR20250041053A (ko) | 2025-03-25 |
| WO2024106362A1 (ja) | 2024-05-23 |
| CN119790228A (zh) | 2025-04-08 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| US12060909B2 (en) | Sliding component | |
| CN115803548B (zh) | 滑动部件 | |
| US12152676B2 (en) | Sliding component | |
| JP7475801B2 (ja) | 摺動部品 | |
| JP2009047040A (ja) | スクロール型流体機械 | |
| JP7497132B2 (ja) | 摺動部品 | |
| EP4621235A1 (en) | Thrust support mechanism | |
| KR102744361B1 (ko) | 슬라이딩 부품 | |
| EP4621234A1 (en) | Regulating component | |
| EP4696891A1 (en) | Sliding component | |
| EP4621233A1 (en) | Thrust receiving mechanism | |
| US12110923B2 (en) | Sliding component |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: THE INTERNATIONAL PUBLICATION HAS BEEN MADE |
|
| PUAI | Public reference made under article 153(3) epc to a published international application that has entered the european phase |
Free format text: ORIGINAL CODE: 0009012 |
|
| STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: REQUEST FOR EXAMINATION WAS MADE |
|
| 17P | Request for examination filed |
Effective date: 20250225 |
|
| AK | Designated contracting states |
Kind code of ref document: A1 Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC ME MK MT NL NO PL PT RO RS SE SI SK SM TR |
|
| STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: THE APPLICATION HAS BEEN WITHDRAWN |
|
| DAV | Request for validation of the european patent (deleted) | ||
| DAX | Request for extension of the european patent (deleted) | ||
| 18W | Application withdrawn |
Effective date: 20260130 |